EDGE™ Preliminary Project Plan P09102 – METEOR Stage Separation System JJ Guerrette (ME)

Slides:



Advertisements
Similar presentations
EDGE™ Concept Level Project Plan P09102 – METEOR Stage Separation System JJ Guerrette (ME)
Advertisements

RockSat-C 2012 CoDR Minnesota Sound Wreckers Conceptual Design Review University of Minnesota Alexander Richman Jacob Schultz Justine Topel Will Thorson.
EDGE™ Concept Level Project Plan P08210/11 – Ruggedization of a Data Recorder for a Forklift Truck Shadle Stewart ME Rick Chadwick ME.
Chapter 2.
EDGE™ Copyright © 2007 Rochester Institute of Technology All rights reserved.. Design, Fabrication, and Testing of a Novel, Automated, Remotely Operated.
Daniel Graves (ME). Open Architecture, Open Source Unmanned Aerial Vehicle for Imaging Systems  Primary Customer: RIT College of Imaging Science ○ Currently.
1. P09203 – 1kg Robotic Motor Module Gen 2 Platform This project is Sponsored by the Kate Gleason Foundation.  Team Members:  Lauren Farnsworth → Team.
EDGE™ Preliminary Project Overview P09123 – MAV Platform Team Members: Joe Hozdic (Lead)Ming Chow Aaron NashBrian David Giovanni Sorrentino.
EDGE™ Concept Level Project Plan P08110 – UAV Based Digital Imaging System David Eells (Mechanical Engineering)
Designing new systems or modifying existing ones should always be aimed at helping an organization achieve its goals State the purpose of systems design.
EDGE™ Concept Level Project Plan P08043 – Magnet Centering Device Aaaron Burger (Mechanical Engineer)
Global Procurement Solutions (GPS) Manager of Business Development Final Project, Fall semester December 16, 2000.
P07109: Project M.E.T.E.O.R. Flying Rocket Team Andrew ScarlataProject Leader/ Mechanical Engineer Geoff CassellLead Engineer/ Mechanical Engineer David.
Project Status Update II R09230: Open Architecture, Open Source Unmanned Aerial Vehicle for Imaging Systems A. Benjamin Wager (ME) B. Michael Skube (ME)
EDGE™ Concept Level Project Plan P08110 – UAV Based Digital Imaging System David Eells (Mechanical Engineering)
EDGE™ Concept Level Project Plan P08210/11 – Ruggedization of a Data Recorder for a Forklift Truck Shadle Stewart ME Rick Chadwick ME.
EDGE™ Concept Level Project Plan P08428 – LED Lighting Technologies Courtney Walsh (ME)
EDGE™ Project Status Update P09141 – Thermal Heater Control System Anthony Berwin (Mechanical Engineer)
EDGE™ Final Project Plan P09123 – MAV Platform Structure Joe Hozdic (Mechanical Engineering)
R I T Advisors: Dr. Wayne WalterMechanical Engineering Dept. Faculty Jeffrey WebbTeacher’s Assistant Team Members: Aman Verma EE - Electrical Craftsman.
EDGE™ Concept Level Project Plan P09452 Compressor Part Fabrication and ReVamp Snehapriya Rao (ME) Ed Budriss (ME) Alex Scarangella (ME) Edward Wolf (CE)
PROJECT ICARUS by Noah Michael, Student Project Manager & Dr. Nikos Mourtos, Faculty Project Manager AE 170A/B Course Instructor.
METEOR BACKGROUND This is a foundation project in an ambitious endeavor to provide the RIT research community with a means to conduct near space.
Michelle Bard (ME) Alexander Ship (ME) David Monahan (ME) Kristin Gagliardi (ME) October 12, 2009.
ME Project: Air Conditioner Lab Team: 10 Members: Sean M. Gallagher, Brian Davison, Prathana Vannarath, Pam McDowell Customer: University of Delaware Mechanical.
EDGE™ Final Project Presentation P09141 – Satellite Thermal Heater Controller Anthony Berwin (Mechanical Engineer)
EDGE™ Project Status Update P09141 – Satellite Thermal Heater Control System Anthony Berwin (Mechanical Engineer)
P07109: Project M.E.T.E.O.R. Flying Rocket Team Andrew ScarlataProject Leader/ Mechanical Engineer Geoff CassellLead Engineer/ Mechanical Engineer David.
Icarus Student Satellite Project
P /20093 Composites Autoclave Brandon Allen (EE) Matt Brady (ME) Brian Cario (ME) Matt DiFrancesco (ME) John Mink (EE) ‏ Chris DeMinco.
Analyzing the Business Case
EDGE™ Project Status Update P09121 – MAV Airframe P09122 – MAV Control System P09123 – MAV Platform Structure Aaron Nash (Mechanical Engineering) Erik.
Project METEOR Microsystems Engineering and Technology for the Exploration of Outer Regions.
Christopher Barrett (ME) Daniel Graves (ME). Open Architecture, Open Source Unmanned Aerial Vehicle for Imaging Systems Primary Customer: ○ Currently.
Sponsored by Wegmans P Automation/Improvement of Packaging on the Cookie Line Stephanie Rager Bruno Coelho.
Miscellaneous Notes: This is a bare-bones template – make it fancier if you wish, but be sure to address at least the items listed here. Basically this.
Proposed Approach  Research available commercial satellite communications services  Explore viable battery technologies  Investigate GPS receiver functionality.
Chapter 3 Dr. Bahaa Al-Sheikh & Eng. Mohammed Al-Sumady Intoduction to Engineering Introduction to Engineering Design 1.
TESTING LEVELS Unit Testing Integration Testing System Testing Acceptance Testing.
PROJECT STATUS UPDATE P10661-AERIAL IMAGING Dale Turley (Mechanical Engineering)
NASA/Air Force Cost Model presented by Keith Smith Science Applications International Corporation 2002 SCEA National Conference June
through Introduction  Particle Imaging Velocimetry (PIV) uses a sheet laser beam to illuminate particles that cross the sheet.  The particles.
P15080: Flow Culture System Multi-Disciplinary Senior Design Problem Definition Review September 11, 2014 Collin Burkhart – Lead Mechanical Engineer Katelyn.
SOLUTION What kind of plan do we need? How will we know if the work is on track to be done? How quickly can we get this done? How long will this work take.
Haripriya Head, Integration Team Pratham, IIT Bombay 19 th June, 2010.
THROUGH NERANJAN DHARMADASA JAMES BROWN P09451: Thermo-Electric Module for Large Scale Systems.
Tata McGraw CHAPTER 4 Product and Service Design.
EDGE™ Concept Level Project Plan P08210/11 – Ruggedization of a Data Recorder for a Forklift Truck Shadle Stewart ME Rick Chadwick ME.
Project Final Presentation Joe Featherall.
EDGE™ Final Project Plan Presentation P09001 – RFID Reader & Active Tag Philip Davenport (Industrial and Systems Engineering)
EDGE™ Final Project Plan Presentation P08043 – Mass Spectrometry Sample Preparation.
EDGE™ Preliminary Project Plan P09103 Rocket Fail Safe Device Chris Natoli (ME)
P07122: Autonomous Quadcopter Jason Enslin – EE: Team Leader, Circuit Design/Testing Glenn Kitchell – CE: Programming, Software Design Richard Nichols.
Allen Luccitti (ME). Mission Statement Product Description ▫ Test stand consisting of a centrifugal pump, closed loop flow system with control through.
Systems Analysis & Design 7 th Edition Chapter 2.
Project METEOR – R.I.T. Satellites!!. Project METEOR – R.I.T. Overview of Project METEOR: METEOR Video
EDGE™ Concept Level Project Plan P09103 Rocket Self-Destruction Device Chris Natoli (ME)
Microcontroller Enhancement Design Project
Turbomachinery Flow Visualization P08453
Concept Level Project Plan P08008 – ArcWorks Process Improvement
End of DPM Presentation P08405—Novel Materials Technology
Concept Level Project Plan P08453 – Turbomachinery Flow Visualization
Right Move, Right Place, Right Time
Concept Level Project Plan P09102 – METEOR Stage Separation System
P07107: Mission Control Procedures Aerospace Systems and Technology
Project Readiness Review P10029 – Air Muscle Artificial Limb
Satellites!!.
Final Status Update P09006 – Upper Extremity Exerciser
Final Project Plan P09004 – Eye Movement Tracking Device
GOLD-2 – Anticipating Customer Needs
Presentation transcript:

EDGE™ Preliminary Project Plan P09102 – METEOR Stage Separation System JJ Guerrette (ME)

EDGE™ Product Description This project will provide Project METEOR with a stage separation system (SSS). The project scope includes a mechanical device and electronic control system to precisely time the stage separation sequences. Key Business Goals This project will provide the students and faculty at RIT, and the scientific community at large, the opportunity to obtain small payload volumes for conducting micro-systems and other scientific experiments in outer space. METEOR will accommodate and promote these multi-disciplinary collaborations. The final product holds the potential to attract universities aimed at space-based research and satellite sciences. Primary Market The RIT scientific community and Project METEOR Secondary Market Universities looking to launch satellites weighing less than 1kg into space for a low cost Stakeholders METEOR Faculty Guides as customers Harris Corporation as a financier RIT Students and Faculty as customers NASA as a possible financier Universities with Space Research Programs as customers Aerospace Companies as possible financiers or competitors Phase 0: Planning Mission Statement

EDGE™ Phase 1: Concept Development Customer Needs METEOR Needs 1. Needs to deliver a 1kg payload to LEO 2. Needs to be controllable and semi-autonomous 3. Needs to have a planned trajectory 4. Needs to be safe to the operator 5. Needs to be a cost effective alternative to current launch methods 6. Needs to be safe for community surrounding the launch site 7. Needs to have a (propellant) : (structure) ratio of 10:1 and a total mass around ~200kg 8. Needs to integrate multiple projects and systems SSS Needs 1. Needs to enable the separation of rocket stages 2. Needs to hold rocket stages together until separation 3. Needs to be lightweight 4. Needs to be robust enough to withstand external stresses 5. Needs to have minimal effect on the rocket trajectory 6. Needs to remain attached to lower stage in order to reduce the mass of upper stages 7. Needs to be testable on the ground and at altitude 8. Needs to bridge hardwired communications between stages 9. Needs to be precisely timed with control algorithms 10. Needs to integrate with the METEOR guidance system 11. Needs to integrate with the METEOR rocket body 12. Needs to operate in a vacuum 13. Needs to perform in altitudes from sea level to1200mi 14. Needs to be used only once 15. Needs to be scalable

EDGE™ METEOR Stage Separation System Constraints 20 Weeks METEOR Systems Integration Guidance System Rocket Body Lightweight Minimal effect on trajectory Resources Patru and Kozak METEOR Lab Previous SD websites Economics Unknown Budget Cost-effective alternative Scope Stage Separator Stage Connector Inter-Stage Communications Scalable Single cycle life Technology Control Algorithms Optical Connections Lightweight Materials Phase 1: Concept Development Objective Tree

EDGE™ Affinity Diagram

EDGE™ Phase 0: Planning Staffing Requirements Mechanical Engineers 3 The mechanical engineers will be tasked with parts fabrication, material acquisition, and the design of a release mechanism. They will create a dynamic model of the stage separation sequence. They will design a method of integrating the system with the rocket-body. They will ensure that all materials used in the system are compatible. Electrical Engineers 2 The electrical engineers will purchase and integrate the system’s controller with the METEOR guidance system. This may also include the purchase of a transmitter and receiver for communications. They will determine power requirements of the SSS. EE’s will develop control algorithms for the separation events, including writing code. The EE’s will investigate optical devices for inter-stage communication. Industrial and Systems Engineers 1 Requirements flow-down from customer needs to product specifications. They will design the test procedures to make sure the system meets all customer needs. Computer Engineers 0 Business Majors 0

EDGE™ Staffing Requirements

EDGE™ Phase 0: Planning Resource Requirements People -Current METEOR SD teams and Dr. Patru and Dr. Kozak will have more information at the start of the project. Equipment Will an environmental chamber be necessary? Can the system be designed around it? Materials Controllers compatible with the METEOR guidance system will need to be purchased.

EDGE™ Phase 1: Concept Development Identify Customer Needs - Benchmarking Stage Separation Devices: (Swiss Propulsion Labs) Source: NEA’s separation ring is reusable and uses a quick release mechanism. Reusability is not important for the METEOR SSS. Small electronic actuators could be used. SPL’s solution is robust and reusable. One downside to the use of a robust mechanical system is the added weight of the components.

EDGE™ Future Plan I need to estimate the number of hours for each work item and create a preliminary work breakdown structure. I also need to talk to Dr. Crassidis about control systems design. I’d like to have one more meeting with Dr. Kozak and Dr. Patru to make sure that I have METEOR’s needs correct.